On-Line Trajectory Generation Method Based on Closed-Form Analytical Solution for Reusable Launch Vehicle.
Autor: | LI Zhao-ying1 lizhaoying@buaa.edu.cn, HUANG Xing-li2, LI Hui-feng1 |
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Zdroj: | Journal of Astronautics / Yuhang Xuebao. Jun2013, Vol. 34 Issue 6, p755-762. 8p. |
Databáze: | Academic Search Ultimate |
Externí odkaz: |